Aerodynamics of inter-spool duct under the influence of an upstream transonic compressor stage-Reference-Cited by-同舟云学术

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Aerodynamics of inter-spool duct under the influence of an upstream transonic compressor stage

Published:2023-06 Issue: Volume:137 Page:108282
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Kumar Lakshya^ORCID,Alone Dilipkumar B,A M Pradeep^ORCID

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference29 articles.

1. Engine architecture for high efficiency at small core size;Lord,2015

2. Gas Turbine Theory;Saravanamuttoo,2001

3. Fundamentals of Jet Propulsion with Applications;Flack,2005

4. Effect of length on compressor inter-stage duct performance;Ortiz Dueñas,2007

5. Effect of inlet conditions on compressor intermediate duct;Gao;Proc. Inst. Mech. Eng., G J. Aerosp. Eng.,2014

Cited by 4 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Investigation of Transonic Flow Features in an Axial Flow Compressor Rotor;Defence Science Journal;2024-03-26

2. Shock Dynamics and Associated Flow Physics at Near Stall Condition in a Transonic Axial Flow Compressor Stage;International Journal of Gas Turbine, Propulsion and Power Systems;2024

3. Evolution of unsteady secondary flow structures near the onset of stall in a tip-critical transonic axial flow compressor stage;Physics of Fluids;2023-10-01

4. A study of the effect of curvature and pressure gradient on aerodynamics performance and turbulence structure of S-shaped compressor transition duct;Australian Journal of Mechanical Engineering;2023-07-05

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